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Aircraft New Tire Standard - Bias and Radial

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • AS4833A
  • Current
Published 2019-10-17 by SAE International in United States
This SAE Aerospace Standard (AS) sets forth criteria for the selection and verification processes to be followed in providing tires that will be suitable for intended use on civil aircraft. This document encompasses new and requalified radial and bias aircraft tires.
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Tire Burst Test Methodology

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6265
  • Current
Published 2019-10-17 by SAE International in United States
This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanes.
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Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base

AMS J Aircraft Maintenance Chemicals and Materials Committee
  • Aerospace Material Specification
  • AMS1523B
  • Current
Published 2019-06-03 by SAE International in United States
This specification covers a thickened, water-base, type cleaner in the form of a gel.
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Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-Base

AMS J Aircraft Maintenance Chemicals and Materials Committee
  • Aerospace Material Specification
  • AMS1533C
  • Current
Published 2019-01-08 by SAE International in United States
This specification covers a solvent-base cleaner in the form of a gel.
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Aircraft Lightning Zone

AE-2 Lightning Committee
  • Aerospace Standard
  • ARP5414B
  • Current
Published 2018-12-05 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) defines lightning strike zones and provides guidelines for locating them on particular aircraft, together with examples. The zone definitions and location guidelines described herein are applicable to Parts 23, 25, 27, and 29 aircraft. The zone location guidelines and examples are representative of in-flight lightning exposures.
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Landing and Taxiing Lights - Design Criteria for Installation

A-20B Exterior Lighting Committee
  • Aerospace Standard
  • ARP693E
  • Current
Published 2018-07-02 by SAE International in United States
This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a Single engine personal and/or liaison type b Light twin engine c Large multiengine propeller d Large multiengine turbojet/turbofan e Military high-performance fighter and attack f Helicopter This document will cover general requirements and recommended practices for all types of landing and taxi lights. More specific recommendations for LED lights in particular can be found in ARP6402.
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Stretchable Mesh for Cavity Noise Reduction

  • Magazine Article
  • TBMG-28565
Published 2018-03-01 by Tech Briefs Media Group in United States

NASA’s Langley Research Center has developed a landing gear cavity modification that reduces noise produced during aircraft approach and landing. The modification is an innovative stretchable mesh assembly that deploys and retracts with the landing gear to reduce high-intensity low- to mid-frequency airframe noise. The envisioned low-profile mesh concept enables mitigation of cavity noise without sealing of the cavity or incurring appreciable penalties of increased weight, and conforms easily and smoothly to the interior edges of an aircraft wheel well. The concept is potentially suitable for retrofit of current aircraft and for inclusion into future civil transport fleets, and causes no adverse effects to the aerodynamic characteristics of the aircraft. The technology has been validated in wind tunnel testing. NASA is seeking partners who are interested in co-development or licensure of the technology for a variety of applications.

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Mechanical Switch Usage for Landing Gear Applications

A-5B Gears, Struts and Couplings Committee
  • Aerospace Standard
  • AIR4077
  • Current
Published 2017-10-18 by SAE International in United States
This Aerospace Information Report (AIR) will examine considerations relative to the use of mechanical switches on aircraft landing gear, and present "lessons learned" during the period that these devices have been used.
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Tire Spray Suppression - Airplane Design and Consideration for

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR1904B
  • Current
Published 2017-05-09 by SAE International in United States
This SAE Aerospace Information Report (AIR) relates considerations for design test procedures and test data evaluation for qualification of tire spray deflection devices.
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Use of Structural Carbon Heat Sink Brakes on Aircraft

A-5A Wheels, Brakes and Skid Controls Committee
  • Aerospace Standard
  • AIR1934A
  • Current
Published 2016-11-15 by SAE International in United States
The purpose of this document is to relate areas where carbon brake technology may differ from traditional steel brake technology in design and performance. Carbon brakes have been used on military aircraft for many years and are now frequently used on newly commercial developed aircraft. This document presents some of the lessons learned.
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